Lift-drag ratio of a hypersonic waverider of delta planform

DOI10.1007/BF03374538zbMath0922.76236OpenAlexW2498492136MaRDI QIDQ1280529

A. A. Chulkov, M. A. Zubin, N. A. Ostapenko

Publication date: 14 October 1999

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf03374538

zbMATH Keywords

boundary layer flowisoperimetric conditionsshock layeraerodynamic loadsviscous interactioneffect of aperture angle

Mathematics Subject Classification ID

Hypersonic flows (76K05)

Cites Work

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• Optimization of the spatial shape of load-carrying bodies of small elongation at hypersonic velocities
• Experimental study of aerodynamic for three-dimensional bodies with a star-shaped cross-sections at super- and hypersonic speeds
• Aerodynamic characteristics of \(V\)-shaped wings with shock waves detached from leading edges at hypersonic speeds
• Simulation of the aerodynamic drag of three-dimensional star-shaped bodies at hypersonic velocities
• Lifting wings of optimum shape in a viscous hypersonic stream